AIRPLANE FLIGHT MANUAL SUPPLEMENT E-2708 MT-PROPELLER MODEL - - PDF document

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MT-Propeller Entwicklung GmbH Flugplatzstr.1 94348 Atting GERMANY AIRPLANE FLIGHT MANUAL SUPPLEMENT E-2708 MT-PROPELLER MODEL MTV-6-A/190-69 ON DR400 Series with Engine TAE-125-114 installed per EASA STC 10014219 Serial No.

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Revision 1 – 22 September 2015 Page 1 of 13

Form E-1346

MT-Propeller Entwicklung GmbH Flugplatzstr.1 94348 Atting GERMANY

AIRPLANE FLIGHT MANUAL SUPPLEMENT E-2708 MT-PROPELLER MODEL MTV-6-A/190-69 ON DR400 Series with Engine TAE-125-114 installed per EASA STC 10014219 Serial No. Registration No.

This supplement must be attached to the Section 9 of the Pilot´s Operating Handbook and approved Airplane Flight Manual upon installation of the MT-Propeller Model MTV-6-A/190-69. The information contained in this document supplements or supersedes the information of the Pilot´s Operating Handbook and approved Airplane Flight Manual and appropriate Airplane Flight Manual Supplements only in those areas listed. For Limitations, Procedures, and Performance Data not contained in this supplement, consult the Pilot´s Operating Handbook and approved Airplane Flight Manual and appropriate Airplane Flight Manual Supplements. The technical content of this document is approved under the authority of DOA No. EASA.21J.020 Published By: MT-Propeller Entwicklung GmbH (DOA No. EASA.21J.020) D-94348 Atting, Germany

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation Aircraft Flight Manual Supplement Log of revisions Rev. No. Page Revised Description of Revision Date Approved by All Initial Issue 10 September 2015 EASA 1 1, 2, 4, 6 Editorial Change 22 September 2015 A black bar in the margin of a revised page shows the current change.

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation Table of Contents SECTION 1 – GENERAL PAGE 4 SECTION 2 – LIMITATIONS PAGE 6 SECTION 3 – EMERGENCY PROCEDURES PAGE 7 SECTION 4 – NORMAL PROCEDURES PAGE 7 SECTION 5 – PERFORMANCE PAGE 7 SECTION 6 – WEIGHT AND BALANCE AND EQUIPMENT LIST PAGE 8 SECTION 7 – DESCRIPTION OF THE AIRCRAFT AND ITS SYSTEMS PAGE 8 SECTION 8 – HANDLING, SERVICE & MAINTENANCE PAGE 9 SECTION 9 – SUPPLEMENTS PAGE 9 SECTION 10 – OPERATIONAL TIPS PAGE 9

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation

SECTION 1 - GENERAL

The operator must thoroughly familiarize himself with the airplane and the contents of this supplement before initial operation. Thereafter this manual should be reviewed periodically to enable the operator to maintain the highest level of familiarity with the airplane, its controls and recommended operating procedures. ENGINE(S) Number of Engines: 1 Manufacturer: Technify Motors GmbH Engine Models:

TAE-125-114 installed per EASA STC 10014219

PROPELLER(S) Number of Propellers: 1 Manufacturer: MT-Propeller Entwicklung GmbH, Germany Propeller Model: MTV-6-A/190-69 Number of Blades: 3 Propeller Diameter: 190 cm (74.8 in) Propeller Type: Constant-speed, hydraulically actuated Blade Angles: Measured at the 71 cm (28 in) station: Low Pitch: +13,5° ±0,2° High Pitch: +28° ±1° EASA TCDS No.: P.094 FAA TCDS No.: P19NE

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation

SECTION 1 – GENERAL continued

NOISE LEVELS European registered aircrafts The noise levels will be listed in the database of EASA approved noise levels for light propeller driven airplanes, latest issue and have been verified and approved by EASA. The noise tests were conducted in accordance with ICAO Annex 16, Volume 1 (6th edition, July 2011), Chapter 10. U.S. registered aircrafts The corrected noise level of this aircraft with this propeller is equal to or better than production aircrafts. No determination has been made by the Federal Aviation Administration that the noise levels of this aircraft are or should be acceptable or unacceptable for operation at, into, or out of, any airport. ELIGIBILITY AND COMPATIBILITY The eligibility with this modification is given for approved airframe and gross weight configurations which do not affect the propeller/engine configuration.

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation

SECTION 2 – LIMITATIONS

ENGINE(S) Number of Engines: 1 Manufacturer: Technify Motors GmbH Engine Models:

TAE-125-114 installed per EASA STC 10014219

PROPELLER(S) Number of Propellers: 1 Manufacturer: MT-Propeller Entwicklung GmbH, Germany Propeller Model: MTV-6-A/190-69 Propeller Hub: MTV-6-A Propeller Blade: 190-69 Number of Blades: 3 Propeller Diameter: 190 cm (74.8 inches) Cut-off to 185 cm (72.8 inches) allowed for repair. Blade Angles: Measured at the 71 cm (28 in) station: Low Pitch: +13,5° ±0,2° High Pitch: +28° ±1° Propeller Speed Limits (Np): none POWER PLANT LIMITATIONS No change PLACARDS Placards concerning other propellers are obsolete and must be removed or permanently covered.

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation

SECTION 3 - EMERGENCY PROCEDURES

No Change.

SECTION 4 - NORMAL PROCEDURES

No change.

SECTION 5 - PERFORMANCE

When the new MTV-6-A/190-69 propeller is installed the following Data are applicable: Take Off 1100kg: SHORT FIELD TAKEOFF DISTANCE

TOGW= 1100 kg

Speed at Liftoff Vlof = 61 KIAS

2425 lb

Speed over 50 ft Obstacle V50 = 68 KIAS Flaps: Step 1 - Full Throttle, 155HP @ 2300 RPM (at ISA SL) Dry Paved RWY PRESS DISTANCE TEMPERATURE - °C ALT [FT] [m] ISA ISA+10 ISA+20 ISA+30 Gnd Roll 214 231 248 266 50 ft 400 432 466 501 1000 Gnd Roll 226 244 262 282 50 ft 423 457 492 530 2000 Gnd Roll 239 258 277 298 50 ft 447 483 521 560 3000 Gnd Roll 253 273 294 315 50 ft 473 511 551 593 4000 Gnd Roll 268 289 311 334 50 ft 501 541 583 628 5000 Gnd Roll 284 306 329 354 50 ft 531 573 618 665 6000 Gnd Roll 301 324 349 375 50 ft 562 607 655 704 7000 Gnd Roll 322 347 373 401 50 ft 603 651 702 756 8000 Gnd Roll 345 372 400 430 50 ft 648 699 754 811

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation

SECTION 5 – PERFORMANCE (Continued)

Take Off 1000kg: SHORT FIELD TAKEOFF DISTANCE

TOGW= 1000 kg

Speed at Liftoff Vlof = 59 KIAS

2205 lb

Speed over 50 ft Obstacle V50 = 63 KIAS Flaps: Step 1 - Full Throttle, 155HP @ 2300 RPM (at ISA SL) Dry Paved RWY PRESS DISTANCE TEMPERATURE - °C ALT [FT] [m] ISA ISA+10 ISA+20 ISA+30 Gnd Roll 167 180 194 208 50 ft 312 337 363 391 1000 Gnd Roll 177 190 205 220 50 ft 330 356 384 413 2000 Gnd Roll 187 201 217 233 50 ft 349 377 406 437 3000 Gnd Roll 198 213 229 246 50 ft 370 399 430 463 4000 Gnd Roll 209 225 243 261 50 ft 391 422 455 490 5000 Gnd Roll 222 239 257 276 50 ft 414 447 482 519 6000 Gnd Roll 235 253 272 292 50 ft 439 474 511 550 7000 Gnd Roll 251 271 292 313 50 ft 471 508 548 590 8000 Gnd Roll 269 290 312 335 50 ft 506 546 589 633

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation

SECTION 5 – PERFORMANCE (Continued)

Climb 1100kg

TIME, FUEL, AND DISTANCE TO CLIMB, Enroute Climb

Associated Conditions:

TOW= 1100 kg

Standard Day(ISA)

2425 lb

Power: full throttle Flaps: Clean Note: Distances shown are based on zero wind add appropriate 4l for startup and taxi Press.Alt. OAT Vy ROC Time Distance Fuel used [FT] [°C] [KIAS] [FPM] [MIN] [NAM] [ l ] 15 78 740 0,0 0,0 0,0 1000 13 78 730 1,4 1,8 0,8 2000 11 78 720 2,7 3,7 1,5 3000 9 78 710 4,1 5,6 2,3 4000 7 78 700 5,6 7,7 3,1 5000 5 78 690 7,0 9,8 3,9 6000 3 78 679 8,5 12,0 4,7 7000 1 78 668 9,9 14,3 5,6 8000

78 656 11,5 16,8 6,5 9000

78 606 13,0 19,4 7,3 10000

75 545 14,8 21,5 8,3 11000

75 484 16,7 24,7 9,3 12000

75 423 18,9 28,4 10,4 13000

72 362 21,5 31,4 11,6 14000

72 300 24,5 36,4 13,0 15000

72 238 28,2 42,7 14,7 16000

72 175 33,1 50,8 16,7 17000

72 112 40,0 62,5 19,4

RATE OF CLIMB

Associated Conditions:

MTOW = 1100 kg = 2425 lb

Power: full throttle Flaps: Clean Notes:

1. For operation in air colder than this table provides, use coldest data shown
2. For operation in air warmer than this table provides, use extreme caution

Press. ISA Climb RATE OF CLIMB - Feet per Minute Alt. OAT Speed Temperature - °C [FT] [ ° C] [KIAS] ISA ISA+10 ISA+20 ISA+30 15 78 740 701 662 623 1000 13 78 730 691 652 613 2000 11 78 720 681 641 602 3000 9 78 710 670 631 591 4000 7 78 700 660 620 580 5000 5 78 690 649 609 569 6000 3 78 679 638 597 557 7000 1 78 668 627 586 545 8000

78 656 615 574 533 9000

78 606 565 524 484 10000

75 545 505 465 425 11000

75 484 445 405 366 12000

75 423 384 345 307 13000

72 362 323 285 247 14000

72 300 262 225 188 15000

72 238 201 164 127 16000

72 175 139 103 67 17000

72 112 77 41 6

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation

SECTION 5 – PERFORMANCE (Continued)

Climb 1000kg

TIME, FUEL, AND DISTANCE TO CLIMB, Enroute Climb

Associated Conditions:

TOW= 1000 kg

Standard Day(ISA)

2205 lb

Power: full throttle Flaps: Clean Note: Distances shown are based on zero wind add appropriate 4l for startup and taxi Press.Alt. OAT Vy ROC Time Distance Fuel used [FT] [°C] [KIAS] [FPM] [MIN] [NAM] [ l ] 15 78 910 0,0 0,0 0,0 1000 13 78 901 1,1 1,5 0,6 2000 11 78 891 2,2 3,0 1,2 3000 9 78 882 3,3 4,5 1,9 4000 7 78 872 4,5 6,2 2,5 5000 5 78 862 5,6 7,9 3,2 6000 3 78 852 6,8 9,7 3,8 7000 1 78 841 8,0 11,5 4,5 8000

78 830 9,2 13,5 5,2 9000

78 776 10,4 15,5 5,9 10000

75 711 11,8 17,1 6,6 11000

75 646 13,3 19,6 7,4 12000

75 581 14,9 22,3 8,2 13000

72 515 16,7 24,5 9,1 14000

72 449 18,8 27,9 10,0 15000

72 382 21,2 32,0 11,1 16000

72 316 24,1 37,0 12,3 17000

72 249 27,6 43,1 13,7

RATE OF CLIMB

Associated Conditions:

MTOW = 1000 kg = 2205 lb

Power: full throttle Flaps: Clean Notes:

1. For operation in air colder than this table provides, use coldest data shown
2. For operation in air warmer than this table provides, use extreme caution

Press. ISA Climb RATE OF CLIMB - Feet per Minute Alt. OAT Speed Temperature - °C [FT] [ ° C] [KIAS] ISA ISA+10 ISA+20 ISA+30 15 78 910 869 827 786 1000 13 78 901 859 818 776 2000 11 78 891 849 808 766 3000 9 78 882 840 798 756 4000 7 78 872 829 787 745 5000 5 78 862 819 777 734 6000 3 78 852 809 766 723 7000 1 78 841 798 755 712 8000

78 830 787 743 700 9000

78 776 733 691 648 10000

75 711 669 627 586 11000

75 646 605 564 523 12000

75 581 540 500 459 13000

72 515 475 435 396 14000

72 449 410 371 332 15000

72 382 344 306 268 16000

72 316 278 240 203 17000

72 249 212 175 138

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation

SECTION 5 – PERFORMANCE (Continued)

All other performance have been determined to be equal to or better than the baseline

airplane. Therefore allother performance data from the baseline aircraft can be used for

performance determination.

SECTION 6 - WEIGHT AND BALANCE AND EQUIPMENT LIST

The new MTV-6-A/190-69 has the same Weight and CG as the original MTV-6-A/187-129. When installing the MTV-6-A/190-69 propeller, the equipment list must be amended to reflect addition of this propeller.

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation

SECTION 7 - DESCRIPTION OF THE AIRCRAFT AND ITS SYSTEMS

Propeller: The MTV-6-A/190-69 is a 3-blade hydraulically actuated, constant speed propeller with 190 cm (74.8 in) diameter. The propeller construction consists of natural composite blades mounted in a conventional aluminum hub. Stainless steel erosion sheaths protect the propeller blade leading edges. The propeller is driven by the engine via a reduction gear box.. The propeller pitch and speed control is maintained by oil pressure via an ECU controlled Constant Speed Unit. An internal spring moves the propeller blades towards the low pitch (high rpm), while the CSU controlled oil pressure, moves the propeller blades towards high pitch (low rpm). The CSU uses gearbox oil for propeller control. CAUTION Do not push aircraft on spinner.

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Form E-1346

MT-Propeller Entwicklung GmbH AFM Supplement Doc. No. E-2708 Flugplatzstr.1 DR 400 Series 94348 Atting MTV-6-A/190-69 GERMANY Propeller Installation

SECTION 8 – HANDLING, SERVICE & MAINTENANCE

Propeller Service: Since the MT-Propellers may also pick up loose pieces of rock and debris from the ramp and runway, the blades should be checked prior to each flight for damage. The daily preflight is performed by the pilot and includes examination of the propeller blades and spinners for visible damage, cracks, grease or oil leakage, blade shake and blade angle

play. Blade shake up to 1/8 inches (3 mm) and a blade angle play of 2° is allowed.

Do not dress out prop nicks. Maintenance and repairs should only be accomplished by appropriately rated and qualified personnel in accordance with MT-Propeller´s Instruction for Continued Airworthiness Doc. No. E-2710, latest revision. The propellers may be cleaned with a mild solution of soap and water. Do not use solvents.